| Patents for F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants (30,889) |
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| 06/16/2009 | US7546741 Ignition detecting system and method for gas turbine |
| 06/16/2009 | US7546740 Nozzle |
| 06/16/2009 | US7546739 Igniter tube and method of assembling same |
| 06/16/2009 | US7546736 Methods and apparatus for low emission gas turbine energy generation |
| 06/16/2009 | CA2398248C Diagnostic method and system for turbine engines |
| 06/14/2009 | CA2647152A1 Bearing structure uncoupling device |
| 06/14/2009 | CA2647139A1 Assembly of pressurization tubes in an inner chamber of a turbine engine |
| 06/14/2009 | CA2647058A1 Sealing of a hub cavity in the exhaust casing of a turbine engine |
| 06/14/2009 | CA2646976A1 Bearing bracket sealed fitting in a turbine engine |
| 06/14/2009 | CA2646959A1 Injection system of a fuel and air mixture in a turbine engine combustion system |
| 06/11/2009 | US20090148292 Axial compressor for tip turbine engine |
| 06/11/2009 | US20090148280 Turbine Vane for a Gas Turbine Engine |
| 06/11/2009 | US20090148279 Gas turbine belly band seal anti-rotation structure |
| 06/11/2009 | US20090148276 Seal assembly for a fan rotor of a tip turbine engine |
| 06/11/2009 | US20090148273 Compressor inlet guide vane for tip turbine engine and corresponding control method |
| 06/11/2009 | US20090148271 Bearing mounting system in a low pressure turbine |
| 06/11/2009 | US20090145137 Transition duct assembly |
| 06/11/2009 | US20090145135 Turbine blow down starter for turbine engine |
| 06/11/2009 | US20090145131 Fuel distribution system for a gas turbine with multistage burner arrangement |
| 06/11/2009 | US20090145099 Transition duct cooling feed tubes |
| 06/10/2009 | EP2067986A2 System and method for generating and sustaining a corona electric discharge for igniting a combustible gaseous mixture |
| 06/10/2009 | EP2067965A1 Method and device for starting and stopping gas turbine |
| 06/10/2009 | EP2067964A2 Radial staging method and configuration of a liquid injection system for power plants |
| 06/10/2009 | EP2067963A2 Storage chamber pressure system |
| 06/10/2009 | EP2066890A1 Modulating flow through gas turbine engine cooling system |
| 06/10/2009 | EP1347260B1 Heat exchanger |
| 06/10/2009 | DE10361722B4 Stauluftkanal zur Umgebungsluftzufuhr in einem Flugzeug Ram air duct to the ambient air in an aircraft |
| 06/10/2009 | DE102007059056A1 Supporting disk for guide vane liner of turbine of turbocharger, has set of slots distributedly arranged over circumference of disk, where disk is divided by slots into regions elastically movable to each other in radial direction |
| 06/10/2009 | DE102007058954A1 Gasturbinenölversorgungssystem sowie Verfahren zum Betrieb einer Gasturbinen-Lager-Ölversorgung Gas Turbine oil supply system and method for operating a gas turbine bearing oil supply |
| 06/10/2009 | DE102007058953A1 Lagerkammerdrucksystem Bearing chamber pressure system |
| 06/10/2009 | DE102007057309A1 Hitzeschild und Turbolader mit einem Hitzeschild Heat shield and a turbocharger with a heat shield |
| 06/10/2009 | CN101451467A Air-oil separator |
| 06/10/2009 | CN100497903C Combustor of gas turbine |
| 06/09/2009 | US7544043 Turbulator on the underside of a turbine blade tip turn and related method |
| 06/09/2009 | US7544040 Support structure in a turbine or compressor device and a method for assembling the structure |
| 06/09/2009 | US7543777 Air guiding flap of an aircraft comprising control of the pressure forces impinging thereon, process for adjusting the position of an air guiding flap and ram air system including such an air guiding flap |
| 06/09/2009 | US7543442 Turbojet engine comprising a connector arm for ancillary systems, and the connector arm for ancillary systems |
| 06/09/2009 | US7543440 Multiple turbine system with a single recuperator |
| 06/09/2009 | US7543439 Generator assembly |
| 06/09/2009 | CA2626439C Preferential multihole combustor liner |
| 06/09/2009 | CA2514257C Improved configuration and process for carbonyl removal |
| 06/09/2009 | CA2494736C Fan case design with metal foam between kevlar |
| 06/09/2009 | CA2455266C Methods for replacing a portion of a combustor dome assembly |
| 06/09/2009 | CA2453026C Methods for replacing portions of turbine shroud supports |
| 06/09/2009 | CA2382390C Air inlet duct and flying apparatus, especially a missile, equipped with such duct |
| 06/09/2009 | CA2356328C Jet engine nose inlet cowl having de-icing means |
| 06/09/2009 | CA2195859C Microcomponent sheet architecture |
| 06/07/2009 | CA2647223A1 Suspension of a turbojet to an aircraft |
| 06/07/2009 | CA2638592A1 Compact bearing support |
| 06/04/2009 | WO2009069443A1 Composite-type coal gasification power plant facility |
| 06/04/2009 | WO2009069426A1 Combustion burner |
| 06/04/2009 | WO2009068807A2 Method for controlling thermal effluents generated by an aircraft and cooling device for an aircraft implementing said method |
| 06/04/2009 | WO2009068460A1 Heat shield and turbocharger having a heat shield |
| 06/04/2009 | US20090140497 Flexible seal for gas turbine engine system |
| 06/04/2009 | US20090140104 Turbojet nacelle and method for controlling separation in a turbojet nacelle |
| 06/04/2009 | US20090139243 Gas turbine engine with pylon mounted accessory drive |
| 06/04/2009 | US20090139241 Combusting system, remodeling method for combusting system, and fuel injection method for combusting system |
| 06/04/2009 | US20090139200 Turboengine air intake provided with a controlled filter system |
| 06/04/2009 | DE102008037460A1 Im Wesentlichen zylindrische Verbundartikel und Bläsergehäuse Substantially cylindrical composite article and fan case |
| 06/04/2009 | CA2705611A1 Method for controlling thermal effluents generated by an aircraft and cooling device for an aircraft implementing said method |
| 06/03/2009 | EP2065643A2 Combusting system, remodeling method for combusting system, and fuel injection method for combusting system |
| 06/03/2009 | EP2065585A2 Gas turbine engine with pylon mounted accessory drive |
| 06/03/2009 | EP2065568A1 Cooling of a steam turbine |
| 06/03/2009 | EP2065305A1 Air intake for a turboshaft engine equipped with a controlled filtering system |
| 06/03/2009 | EP2064427A1 Intake cone for a jet engine |
| 06/03/2009 | EP1740806B1 Method for continuously operating a liquid conveying device |
| 06/03/2009 | CN201250706Y Mechanism adopting an electromagnetic bearing to be applied to micro internal combustion turbine |
| 06/03/2009 | CN101449039A Gas turbine engine starting method and control device |
| 06/03/2009 | CN101446236A Lubricating and cooling device of rotor bearing of jet engine of microminiature turbine |
| 06/03/2009 | CN101446235A Rotor decoupler system for a gas turbine |
| 06/03/2009 | CN100494759C Device for lubricating component in assembly composed by multi-part |
| 06/02/2009 | US7540157 Internally mounted fuel manifold with support pins |
| 06/02/2009 | US7540155 Thermal shield stone for covering the wall of a combustion chamber, combustion chamber and a gas turbine |
| 06/02/2009 | US7540144 Bleed valve for a gas turbine engine |
| 06/02/2009 | US7540142 Multiple auxiliary power unit system inlet ducts controlled by a single actuator |
| 05/28/2009 | WO2009067048A1 Gas turbine engine |
| 05/28/2009 | WO2009066706A1 Damping device and gas turbine combustor |
| 05/28/2009 | WO2009066103A1 Aircraft engine pylon attachment |
| 05/28/2009 | US20090136342 Duct installation |
| 05/28/2009 | US20090134276 Aircraft firewall |
| 05/28/2009 | US20090133401 Combustor for turbine engine |
| 05/28/2009 | US20090133400 Turbine engine having fuel-cooled air intercooling |
| 05/28/2009 | US20090133380 Gas Turbine Engine |
| 05/28/2009 | US20090133378 Combustion Chamber and Gas Turbine Installation |
| 05/28/2009 | US20090133376 Combined gearbox breather and drain mast for jet aircraft engine |
| 05/28/2009 | DE102008037580A1 Luftentnahmesystem mit internem Verteiler für eine IGCC-Brennkammer und Verfahren Air sampling system with internal distribution for IGCC combustion chamber and procedures |
| 05/27/2009 | EP2063087A2 Fuel staging system |
| 05/27/2009 | EP1327057B1 Device and method for preheating combustibles in combined gas and steam turbine installations |
| 05/27/2009 | CN100491712C Unit for sealing transition region between two parts cool passage of turbomachinery |
| 05/27/2009 | CN100491700C Stator vane actuator in gas turbine engine |
| 05/26/2009 | US7536864 Variable motive nozzle ejector for use with turbine engines |
| 05/26/2009 | US7536850 Emergency fuel shutoff system |
| 05/26/2009 | CA2342033C Method and apparatus for increasing the efficiency of a multi-stage compressor |
| 05/26/2009 | CA2292488C Waste heat recovery in an organic energy converter using an intermediate liquid cycle |
| 05/23/2009 | CA2645233A1 Turbojet engine suspended from a support strut of an aircraft |
| 05/22/2009 | WO2009033579A3 Device for transporting air in a drive system of a vehicle and fuel cell system comprising a device of this type |
| 05/22/2009 | WO2009030987A3 Cooling arrangement of a gas turbine air inlet |
| 05/21/2009 | US20090129916 Turbine apparatus |
| 05/21/2009 | US20090126369 Integrated direct drive starter/generator for turbines |
| 05/21/2009 | US20090126368 Fuel injection system for a gas turbine engine |